The one-dimensional and two-dimensional inverse problems of heat and mass transfer on hypersonic aircraft permeable surfaces

The hypersonic aircraft permeable cylindrical and spherical surfaces effective heat protection mathematical modeling problems are considered. The statements of one- and two-dimensional inverse problems of heat and mass transfer are given. The interpolation and approximation statements of the inverse problems are defined. The computational experiments results are discussed: two types of blowing laws restoration by heat and mass transfer parameters (local heat flow and local friction) for the inverse problem interpolation statement are presented as the examples. The different character of sensitivity of controllable parameters respectively to step changing of control (the blowing) is studied.